Patent · US Active

Integrated heat management for hybrid propulsion

US11292604B2 · kind B2 · utility

3Cited by
5References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateApr 4, 2018
Grant dateApr 5, 2022
Priority date
Expiry dateFeb 22, 2040

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

There is provided a heat management system for a hybrid electrical aircraft comprising electric propulsors powered by a power plant. The heat management system comprises a heat exchanger integrated to a nacelle of at least one of the electric propulsors for dissipating heat withdrawn from the power components of the power plant into ambient air.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.